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This paper presents two simulation studies of problems associated with aircraft automatic landing systems. The specifc control system considered involves the lateral autopilot together with the lateral beam guidance system which aligns the aircraft with the runway. This is not a study of a complete automatic landing system since only motion in the horizontal plane is considered. The simulations have been implemented at the Hybrid Computation Centre of the Technical University of Vienna. using the HYBSYS hybrid simulation processor. These studies provide useful illustrations of the value and practical limitations of some methods currently used for linear control systems design. The article is written in German.
|Keywords:||aircraft, flight control, autopilot, lateral beam guidance system, simulation, hybrid computer|
|Glasgow Author(s) Enlighten ID:||Murray-Smith, Prof David|
|Authors:||Hummer, H., and Murray-Smith, D.J.|
|Subjects:||Q Science > QA Mathematics > QA75 Electronic computers. Computer science|
Q Science > QA Mathematics > QA76 Computer software
T Technology > TL Motor vehicles. Aeronautics. Astronautics
|College/School:||College of Science and Engineering > School of Engineering > Systems Power and Energy|